Chyetverikov ARK-3
The Chyetverikov ARK-3 (ARKtichyeskii - arctic) was a multi-role flying boat designed for Arctic operations that was built in the Soviet Union from 1933. It featured a conventional flying boat hull, with high cantilever wings equipped with floats at mid-span. The two piston engines were mounted in tractor-pusher fashion on a pylon above the fuselage.
| ARK-3 | |
|---|---|
 | |
| Role | Arctic Multi-role Flying Boat |
| National origin | Soviet Union |
| Manufacturer | OKB Chyetverikov |
| Designer | Igor Vyacheslavovich Chyetverikov |
| First flight | 1936 |
| Number built | 7 |
Development
In 1933 Chyetverikov had the design for a compact twin engined flying-boat ready for further development, which he proposed to the Glavsyevmorput (Glavsyevmorput – chief administration of northern sea routes) as a multi-role Arctic aircraft, and an order for a prototype was made, setting up Chyetverikov in his own OKB (design bureau).
The ARK-3 was of mixed construction, with a 14-metre (45.9 ft) long Duralumin stressed skin fuselage; wooden wings of MOS-27 aerofoil section; duralumin tubing tail surfaces; and ailerons with fabric covering. The dual control enclosed cockpit housed two pilots sided by side with two gunners/observers in bow and dorsal positions. Strut-supported wooden floats, at approximately half-span; and a pylon-supported engine nacelle housing tandem radial engines with Townend ring cowlings; completed the structural elements, built with a safety factor of 5.5.
Flight- and sea trials in 1936 revealed weaknesses in the bows, floats and engine nacelle pylon, which were all strengthened. Performance was deemed to be good, prompting an order for a second prototype with the fuselage lengthened by 60 centimetres (24 in) to 14.6 metres (47.9 ft) and a slightly enlarged wing; this was designated ARK-3-2 and the first prototype was re-designated ARK-3-1. A production order for five aircraft was placed, with production commencing immediately.
On 14 July 1937 the ARK-3-1 was destroyed following a structural failure; the ARK-3-2 was destroyed exactly one year later and the programme was cancelled.
Variants
- ARK-3-1
- The first prototype ARK-3 renamed after the second prototype was ordered
- ARK-3-2
- The second prototype ARK-3 with more powerful engines, longer hull, increased wing chord and manual guns fitted in a manual gun turret in the bows and a dorsal sliding hatch.
- ARK-3 MP2
- Designation of the five production aircraft and the initial designation of the first prototype.
Specifications (ARK-3-2)
Data from Gunston, Bill. The Osprey Encyclopaedia of Russian Aircraft 1875 – 1995. London, Osprey. 1995. ISBN 1-85532-405-9
General characteristics
- Crew: 4
- Capacity: 10 pax
- Length: 14.6 m (47 ft 11 in)
- Wingspan: 20 m (65 ft 7.4 in)
- Wing area: 59.5 m2 (640 sq ft)
- Empty weight: 3,642 kg (8,029 lb)
- Gross weight: 5,600 kg (12,346 lb)
- Powerplant: 2 × Shvetsov M-25A , 544.36 kW (730 hp) each
Performance
- Maximum speed: 320 km/h (199 mph, 173 kn)
- Range: 1,500 km (932 mi, 810 nmi)
- Service ceiling: 8,500 m (27,890 ft)
- Rate of climb: 4.76 m/s (937.4 ft/min)
Armament
- 1 x machine gun in a manually operated bow turret.
- 1 x machine-gun in a dorsal sliding hatch
References
- Angelucci, Enzo. The Rand McNally Encyclopedia of Military Aircraft, 1914-1980. San Diego, California: The Military Press, 1983. Pg. 311 ISBN 0-517-41021-4.
- Gunston, Bill. The Osprey Encyclopaedia of Russian Aircraft 1875 – 1995. London, Osprey. 1995. ISBN 1-85532-405-9
- Taylor, Michael J.H. . Jane's Encyclopedia of Aviation. Studio Editions. London. 1989. ISBN 0-517-69186-8